Stress Analysis Report

Analyzed File: QuadCopter Main Body.ipt
Autodesk Inventor Version: 2022 (Build 260153000, 153)
Creation Date: 4/28/2023, 8:10 AM
Study Author: Grace

Static Analysis:1

General objective and settings:

Design Objective Single Point
Study Type Static Analysis
Last Modification Date 4/28/2023, 6:25 AM
Model State Master
Detect and Eliminate Rigid Body Modes No

iProperties

Summary

AuthorGrace

Project

Part NumberQuadCopter Main Body
DesignerGrace
Cost$0.00
Date Created4/27/2023

Status

Design StatusWorkInProgress

Physical

MaterialPC/ABS Plastic
Density0.357273 g/cm^3
Mass0.0489973 kg
Area30992.3 mm^2
Volume137142 mm^3
Center of Gravityx=3.49722 mm
y=-2.25965 mm
z=0.00540883 mm

Note: Physical values could be different from Physical values used by FEA reported below.


Mesh settings:

Avg. Element Size (fraction of model diameter) 0.1
Min. Element Size (fraction of avg. size) 0.2
Grading Factor 1.5
Max. Turn Angle 60 deg
Create Curved Mesh Elements Yes

Material(s)

Name PC/ABS Plastic
General Mass Density 0.357273 g/cm^3
Yield Strength 54.4 MPa
Ultimate Tensile Strength 54.1 MPa
Stress Young's Modulus 2.78 GPa
Poisson's Ratio 0.4 ul
Shear Modulus 0.992857 GPa
Part Name(s) QuadCopter Main Body.ipt

Operating conditions

Force:1

Load Type Force
Magnitude20.000 N
Vector X0.000 N
Vector Y-20.000 N
Vector Z0.000 N
Selected Face(s)

Bearing Load:1

Load Type Bearing Load
Magnitude20.000 N
Vector X0.000 N
Vector Y20.000 N
Vector Z0.000 N
Selected Face(s)

Bearing Load:2

Load Type Bearing Load
Magnitude20.000 N
Vector X0.000 N
Vector Y20.000 N
Vector Z0.000 N
Selected Face(s)

Bearing Load:3

Load Type Bearing Load
Magnitude20.000 N
Vector X0.000 N
Vector Y20.000 N
Vector Z0.000 N
Selected Face(s)

Bearing Load:4

Load Type Bearing Load
Magnitude20.000 N
Vector X0.000 N
Vector Y20.000 N
Vector Z0.000 N
Selected Face(s)

Gravity

Load Type Gravity
Magnitude9810.000 mm/s^2
Vector X0.000 mm/s^2
Vector Y-9810.000 mm/s^2
Vector Z0.000 mm/s^2
Selected Face(s)

Fixed Constraint:1

Constraint Type Fixed Constraint
Selected Face(s)

Results

Reaction Force and Moment on Constraints

Constraint Name Reaction Force Reaction Moment
Magnitude Component (X,Y,Z) Magnitude Component (X,Y,Z)
Fixed Constraint:1 59.5193 N 0 N 0.503288 N m -0.403144 N m
-59.5193 N -0.00839731 N m
0 N -0.301169 N m

Result Summary

Name Minimum Maximum
Volume 137142 mm^3
Mass 0.0489972 kg
Von Mises Stress 0.0111102 MPa 17.2353 MPa
1st Principal Stress -5.53313 MPa 20.0562 MPa
3rd Principal Stress -19.7925 MPa 7.16444 MPa
Displacement 0 mm 3.20985 mm
Safety Factor 3.15632 ul 15 ul

Figures

Von Mises Stress

1st Principal Stress

3rd Principal Stress

Displacement

Safety Factor


C:\Users\Grace\Documents\Inventor\ProjectName\QuadCopter Main Body.ipt